CA3076998A1 - A method for the manufacture of a coated steel sheet - Google Patents
A method for the manufacture of a coated steel sheet Download PDFInfo
- Publication number
- CA3076998A1 CA3076998A1 CA3076998A CA3076998A CA3076998A1 CA 3076998 A1 CA3076998 A1 CA 3076998A1 CA 3076998 A CA3076998 A CA 3076998A CA 3076998 A CA3076998 A CA 3076998A CA 3076998 A1 CA3076998 A1 CA 3076998A1
- Authority
- CA
- Canada
- Prior art keywords
- steel sheet
- anyone
- coating
- zinc
- iron
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 229910000831 Steel Inorganic materials 0.000 title claims abstract description 79
- 239000010959 steel Substances 0.000 title claims abstract description 79
- 238000000034 method Methods 0.000 title claims abstract description 37
- 238000004519 manufacturing process Methods 0.000 title claims abstract description 11
- 238000000576 coating method Methods 0.000 claims description 47
- 239000011248 coating agent Substances 0.000 claims description 46
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 35
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims description 34
- 239000011701 zinc Substances 0.000 claims description 28
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 claims description 23
- 229910052725 zinc Inorganic materials 0.000 claims description 23
- 229910052742 iron Inorganic materials 0.000 claims description 16
- 229910052751 metal Inorganic materials 0.000 claims description 15
- 239000002184 metal Substances 0.000 claims description 15
- 229910052759 nickel Inorganic materials 0.000 claims description 14
- 229910001563 bainite Inorganic materials 0.000 claims description 8
- 238000007669 thermal treatment Methods 0.000 claims description 8
- 229910000734 martensite Inorganic materials 0.000 claims description 7
- 229910052782 aluminium Inorganic materials 0.000 claims description 6
- 239000000203 mixture Substances 0.000 claims description 6
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims description 5
- 238000000137 annealing Methods 0.000 claims description 5
- 229910045601 alloy Inorganic materials 0.000 claims description 4
- 239000000956 alloy Substances 0.000 claims description 4
- 229910001566 austenite Inorganic materials 0.000 claims description 4
- 229910052804 chromium Inorganic materials 0.000 claims description 4
- 239000012535 impurity Substances 0.000 claims description 4
- 229910000859 α-Fe Inorganic materials 0.000 claims description 4
- 229910052750 molybdenum Inorganic materials 0.000 claims description 3
- 229910001567 cementite Inorganic materials 0.000 claims description 2
- KSOKAHYVTMZFBJ-UHFFFAOYSA-N iron;methane Chemical compound C.[Fe].[Fe].[Fe] KSOKAHYVTMZFBJ-UHFFFAOYSA-N 0.000 claims description 2
- 229910001562 pearlite Inorganic materials 0.000 claims description 2
- 229910052719 titanium Inorganic materials 0.000 claims description 2
- 238000003466 welding Methods 0.000 description 14
- 238000005246 galvanizing Methods 0.000 description 13
- 230000004888 barrier function Effects 0.000 description 5
- 238000010438 heat treatment Methods 0.000 description 5
- 238000004626 scanning electron microscopy Methods 0.000 description 4
- 238000004210 cathodic protection Methods 0.000 description 3
- 238000000151 deposition Methods 0.000 description 3
- 229910001338 liquidmetal Inorganic materials 0.000 description 3
- 239000000758 substrate Substances 0.000 description 3
- 229910001335 Galvanized steel Inorganic materials 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000009713 electroplating Methods 0.000 description 2
- 239000008397 galvanized steel Substances 0.000 description 2
- 230000005764 inhibitory process Effects 0.000 description 2
- 229910052748 manganese Inorganic materials 0.000 description 2
- 230000003287 optical effect Effects 0.000 description 2
- 238000000399 optical microscopy Methods 0.000 description 2
- 238000007747 plating Methods 0.000 description 2
- 238000001771 vacuum deposition Methods 0.000 description 2
- 229910052684 Cerium Inorganic materials 0.000 description 1
- 229910001030 Iron–nickel alloy Inorganic materials 0.000 description 1
- 229910001297 Zn alloy Inorganic materials 0.000 description 1
- 239000002390 adhesive tape Substances 0.000 description 1
- 229910000905 alloy phase Inorganic materials 0.000 description 1
- 229910052797 bismuth Inorganic materials 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000003618 dip coating Methods 0.000 description 1
- 229910052746 lanthanum Inorganic materials 0.000 description 1
- 229910052745 lead Inorganic materials 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 238000002791 soaking Methods 0.000 description 1
- 229910052718 tin Inorganic materials 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
- 238000009736 wetting Methods 0.000 description 1
- 229910052726 zirconium Inorganic materials 0.000 description 1
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/012—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of aluminium or an aluminium alloy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B15/00—Layered products comprising a layer of metal
- B32B15/01—Layered products comprising a layer of metal all layers being exclusively metallic
- B32B15/013—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium
- B32B15/015—Layered products comprising a layer of metal all layers being exclusively metallic one layer being formed of an iron alloy or steel, another layer being formed of a metal other than iron or aluminium the said other metal being copper or nickel or an alloy thereof
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/002—Heat treatment of ferrous alloys containing Cr
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/005—Heat treatment of ferrous alloys containing Mn
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D6/00—Heat treatment of ferrous alloys
- C21D6/008—Heat treatment of ferrous alloys containing Si
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D9/00—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor
- C21D9/46—Heat treatment, e.g. annealing, hardening, quenching or tempering, adapted for particular articles; Furnaces therefor for sheet metals
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/22—Ferrous alloys, e.g. steel alloys containing chromium with molybdenum or tungsten
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/34—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of silicon
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C38/00—Ferrous alloys, e.g. steel alloys
- C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
- C22C38/38—Ferrous alloys, e.g. steel alloys containing chromium with more than 1.5% by weight of manganese
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/02—Pretreatment of the material to be coated, e.g. for coating on selected surface areas
- C23C2/022—Pretreatment of the material to be coated, e.g. for coating on selected surface areas by heating
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/04—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the coating material
- C23C2/06—Zinc or cadmium or alloys based thereon
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C2/00—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor
- C23C2/34—Hot-dipping or immersion processes for applying the coating material in the molten state without affecting the shape; Apparatus therefor characterised by the shape of the material to be treated
- C23C2/36—Elongated material
- C23C2/40—Plates; Strips
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/021—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material including at least one metal alloy layer
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/001—Austenite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/002—Bainite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/005—Ferrite
-
- C—CHEMISTRY; METALLURGY
- C21—METALLURGY OF IRON
- C21D—MODIFYING THE PHYSICAL STRUCTURE OF FERROUS METALS; GENERAL DEVICES FOR HEAT TREATMENT OF FERROUS OR NON-FERROUS METALS OR ALLOYS; MAKING METAL MALLEABLE, e.g. BY DECARBURISATION OR TEMPERING
- C21D2211/00—Microstructure comprising significant phases
- C21D2211/008—Martensite
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C28/00—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
- C23C28/02—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material
- C23C28/023—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only
- C23C28/025—Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D only coatings only including layers of metallic material only coatings of metal elements only with at least one zinc-based layer
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- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D7/00—Electroplating characterised by the article coated
- C25D7/06—Wires; Strips; Foils
- C25D7/0614—Strips or foils
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Organic Chemistry (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Crystallography & Structural Chemistry (AREA)
- Heat Treatment Of Sheet Steel (AREA)
- Electroplating Methods And Accessories (AREA)
- Coating With Molten Metal (AREA)
Abstract
The present invention relates a method for the manufacture of a coated steel sheet.
Description
A method for the manufacture of a coated steel sheet The present invention relates to a method for the manufacture of a coated steel sheet. The invention is particularly well suited for the manufacture of automotive vehicles.
Zinc based coatings are generally used because they allow for protection against corrosion, thanks to barrier protection and cathodic protection. The barrier effect is obtained by the application of the metallic coating on steel surface. Thus, the metallic coating prevents the contact between steel and corrosive atmosphere.
The barrier effect is independent from the nature of the coating and the substrate.
On the contrary, sacrificial cathodic protection is based on the fact that zinc is a metal less noble than steel. Thus, if corrosion occurs, zinc is consumed preferentially as compared to steel. Cathodic protection is essential in areas where steel is directly exposed to corrosive atmosphere, like cut edges where surrounding zinc will be consumed before steel.
However, when heating steps are performed on such zinc coated steel sheets, for example hot press hardening or welding, cracks are observed in steel which spread from the steel/coating interface. Indeed, occasionally, there is a reduction of metal mechanical properties due to the presence of cracks in coated steel sheet after above operation. These cracks appear with the following conditions: high temperature; contact with a liquid metal having a low melting point (such as zinc) in addition to the presence of tensile stress; heterogeneous diffusion of molten metal in substrate grain and grain boundaries. The designation for such phenomenon is known as liquid metal embrittlement (LME), also called liquid metal assisted cracking (LMAC).
US2012100391 discloses a method for manufacturing a hot-dip galvanized steel sheet having good plating qualities, plating adhesion and spot weldability, the method comprising:
- coating a base steel sheet with Ni in a coating amount (Cm) of 0.1-1.0 g/m2;
- heating the Ni-coated steel sheet in a reducing atmosphere;
- cooling the heated steel sheet to the temperature (Xs) at which the steel sheet is fed into a galvanizing bath; and - feeding and immersing the cooled steel sheet in the galvanizing bath having an effective Al concentration (CAI) of 0.11-0.14 wt % and a temperature (Tp) of
Zinc based coatings are generally used because they allow for protection against corrosion, thanks to barrier protection and cathodic protection. The barrier effect is obtained by the application of the metallic coating on steel surface. Thus, the metallic coating prevents the contact between steel and corrosive atmosphere.
The barrier effect is independent from the nature of the coating and the substrate.
On the contrary, sacrificial cathodic protection is based on the fact that zinc is a metal less noble than steel. Thus, if corrosion occurs, zinc is consumed preferentially as compared to steel. Cathodic protection is essential in areas where steel is directly exposed to corrosive atmosphere, like cut edges where surrounding zinc will be consumed before steel.
However, when heating steps are performed on such zinc coated steel sheets, for example hot press hardening or welding, cracks are observed in steel which spread from the steel/coating interface. Indeed, occasionally, there is a reduction of metal mechanical properties due to the presence of cracks in coated steel sheet after above operation. These cracks appear with the following conditions: high temperature; contact with a liquid metal having a low melting point (such as zinc) in addition to the presence of tensile stress; heterogeneous diffusion of molten metal in substrate grain and grain boundaries. The designation for such phenomenon is known as liquid metal embrittlement (LME), also called liquid metal assisted cracking (LMAC).
US2012100391 discloses a method for manufacturing a hot-dip galvanized steel sheet having good plating qualities, plating adhesion and spot weldability, the method comprising:
- coating a base steel sheet with Ni in a coating amount (Cm) of 0.1-1.0 g/m2;
- heating the Ni-coated steel sheet in a reducing atmosphere;
- cooling the heated steel sheet to the temperature (Xs) at which the steel sheet is fed into a galvanizing bath; and - feeding and immersing the cooled steel sheet in the galvanizing bath having an effective Al concentration (CAI) of 0.11-0.14 wt % and a temperature (Tp) of
2 460 C., wherein the temperature (Xs) at which the steel sheet is fed into the galvanizing bath satisfies the following relationship: CNi-(Xs-Tp)/2CA1=5-100.
It also discloses a hot-dip galvanized steel sheet wherein the alloy phase is a Fe-Zn alloy phase accounting for 1-20% of the cross-sectional area of the galvanized layer.
However, in the above method, galvanizing was carried out in a bath containing from 0.11 to 0.14wt.% of Al and thus inhibition layer was very week and Fe-Zn intermetallic phases formed. At the industrial scale, this method is difficult to apply since the spot weldability depends on controlling parameters, including the amount of Ni in the coating, the Al concentration of the galvanizing bath, and the difference between the temperature of the galvanizing bath and the temperature at which the steel sheet is fed into the galvanizing bath. Moreover, the spot weldability performed is evaluated based on the electrode life, i.e. the number of continuous welding spots at the time when the nugget diameter reached 4\lt (t:
steel sheet thickness) was measured. There is no mention of a reduction of the presence of cracks in coated steel sheet after the spot welding.
Thus, the object of the invention is to provide a steel sheet coated with a metallic coating which does not have LME issues. It aims to make available, in particular, an easy to implement method in order to obtain a part which does not have LME issues after the forming and/or the welding.
This object is achieved by providing a method according to claim 1. The method can also comprise any characteristics of claims 2 to 18.
Another object is achieved by providing a steel sheet according to claim 19.
The steel sheet can also comprise any characteristics of claims 20 to 25.
Another object is achieved by providing a spot welded joint according to claim 26. The spot welded joint can also comprise characteristics of claims claim 27 to 29.
Finally, another object is achieved by providing the use of the steel sheet or the assembly according to claim 30.
Other characteristics and advantages of the invention will become apparent from the following detailed description of the invention.
It also discloses a hot-dip galvanized steel sheet wherein the alloy phase is a Fe-Zn alloy phase accounting for 1-20% of the cross-sectional area of the galvanized layer.
However, in the above method, galvanizing was carried out in a bath containing from 0.11 to 0.14wt.% of Al and thus inhibition layer was very week and Fe-Zn intermetallic phases formed. At the industrial scale, this method is difficult to apply since the spot weldability depends on controlling parameters, including the amount of Ni in the coating, the Al concentration of the galvanizing bath, and the difference between the temperature of the galvanizing bath and the temperature at which the steel sheet is fed into the galvanizing bath. Moreover, the spot weldability performed is evaluated based on the electrode life, i.e. the number of continuous welding spots at the time when the nugget diameter reached 4\lt (t:
steel sheet thickness) was measured. There is no mention of a reduction of the presence of cracks in coated steel sheet after the spot welding.
Thus, the object of the invention is to provide a steel sheet coated with a metallic coating which does not have LME issues. It aims to make available, in particular, an easy to implement method in order to obtain a part which does not have LME issues after the forming and/or the welding.
This object is achieved by providing a method according to claim 1. The method can also comprise any characteristics of claims 2 to 18.
Another object is achieved by providing a steel sheet according to claim 19.
The steel sheet can also comprise any characteristics of claims 20 to 25.
Another object is achieved by providing a spot welded joint according to claim 26. The spot welded joint can also comprise characteristics of claims claim 27 to 29.
Finally, another object is achieved by providing the use of the steel sheet or the assembly according to claim 30.
Other characteristics and advantages of the invention will become apparent from the following detailed description of the invention.
3 The designation "steel" or "steel sheet" means a steel sheet, a coil, a plate having a composition allowing the part to achieve a tensile strength up to MPa and more preferably up to 2000MPa. For example, the tensile strength is above or equal to 500 MPa, preferably above or equal to 980 MPa, advantageously above or equal to 1180 MPa and even above or equal 1470 MPa.
The invention relates to a method for the manufacture of a coated steel sheet comprising the following step:
A. the provision of a pre-coated steel sheet coating with a first coating comprising iron and nickel, B. the thermal treatment of such pre-coated steel sheet at a temperature between 600 and 1000 C, C. the coating of the steel sheet obtained in step B) with a second coating based on zinc.
Without willing to be bound by any theory, it is an essential feature of the present invention to deposit the first coating of iron and nickel on the sheet steel before the thermal treatment since during the thermal treatment, on the one hand, Ni diffuses towards the steel sheet allowing a Fe-Ni alloy layer. On the other hand, some amount of Ni is still present at the interface between the steel and the coating interface preventing liquid zinc penetration into steel during any heating steps being for example a welding. Thus, by applying the method according to the present invention, it is possible to obtain a barrier layer to LME.
The first coating comprising iron and nickel is deposited by any deposition method known by the person skilled in the art. It can be deposited by vacuum deposition or electro-plating method. Preferably, it is deposited by electro-plating method.
Preferably, in step A), the first coating comprises from 10% to 75%, more preferably between 25 to 65% and advantageously between 40 to 60% by weight of iron.
Preferably, in step A), the first coating comprises from 25 to 90%, preferably from 35 to 75% and advantageously from 40 to 60% by weight of nickel.
In a preferred embodiment, in step A), the first coating consists of iron and nickel.
The invention relates to a method for the manufacture of a coated steel sheet comprising the following step:
A. the provision of a pre-coated steel sheet coating with a first coating comprising iron and nickel, B. the thermal treatment of such pre-coated steel sheet at a temperature between 600 and 1000 C, C. the coating of the steel sheet obtained in step B) with a second coating based on zinc.
Without willing to be bound by any theory, it is an essential feature of the present invention to deposit the first coating of iron and nickel on the sheet steel before the thermal treatment since during the thermal treatment, on the one hand, Ni diffuses towards the steel sheet allowing a Fe-Ni alloy layer. On the other hand, some amount of Ni is still present at the interface between the steel and the coating interface preventing liquid zinc penetration into steel during any heating steps being for example a welding. Thus, by applying the method according to the present invention, it is possible to obtain a barrier layer to LME.
The first coating comprising iron and nickel is deposited by any deposition method known by the person skilled in the art. It can be deposited by vacuum deposition or electro-plating method. Preferably, it is deposited by electro-plating method.
Preferably, in step A), the first coating comprises from 10% to 75%, more preferably between 25 to 65% and advantageously between 40 to 60% by weight of iron.
Preferably, in step A), the first coating comprises from 25 to 90%, preferably from 35 to 75% and advantageously from 40 to 60% by weight of nickel.
In a preferred embodiment, in step A), the first coating consists of iron and nickel.
4 Preferably, in step A), the first coating has a thickness equal or above 0.5 m. More preferably, the first coating has a thickness between 0.8 and 5.0 pm and advantageously between 1.0 and 2.0 m.
Preferably, in step A), the steel sheet composition comprises by weight:
0.10 < C < 0.40%, 1.5< Mn <3.0%, 0.7 < Si <2.0%, 0.05 < Al < 1.0%, 0.75 < (Si+Al) <3.0 %, and on a purely optional basis, one or more elements such as Nb 0.5 A, B 0.005%, Cr 1.0%, Mo 0.50%, Ni 1.0 A, Ti 0.5%, the remainder of the composition making up of iron and inevitable impurities resulting from the elaboration.
Preferably, in step B), the thermal treatment is a continuous annealing. For example, the continuous annealing comprises a heating, a soaking and a cooling step. It can further comprises a pre-heating step.
Advantageously, the thermal treatment is performed in an atmosphere comprising from 1 to 30% of H2 at a dew point between -10 and -60 C. For example, the atmosphere comprises from 1 to 10% of H2 at a dew point between -40 C and -60 C.
Advantageously, in step C), the second layer comprises above 50%, more preferably above 75% of zinc and advantageously above 90% of zinc. The second layer can be deposited by any deposition method known by the man skilled in the art. It can be by hot-dip coating, by vacuum deposition or by electro-galvanizing.
For example, the coating based on zinc comprises from 0.01 to 8.0% Al, optionally 0.2-8.0% Mg, the remainder being Zn.
Preferably, in step A), the steel sheet composition comprises by weight:
0.10 < C < 0.40%, 1.5< Mn <3.0%, 0.7 < Si <2.0%, 0.05 < Al < 1.0%, 0.75 < (Si+Al) <3.0 %, and on a purely optional basis, one or more elements such as Nb 0.5 A, B 0.005%, Cr 1.0%, Mo 0.50%, Ni 1.0 A, Ti 0.5%, the remainder of the composition making up of iron and inevitable impurities resulting from the elaboration.
Preferably, in step B), the thermal treatment is a continuous annealing. For example, the continuous annealing comprises a heating, a soaking and a cooling step. It can further comprises a pre-heating step.
Advantageously, the thermal treatment is performed in an atmosphere comprising from 1 to 30% of H2 at a dew point between -10 and -60 C. For example, the atmosphere comprises from 1 to 10% of H2 at a dew point between -40 C and -60 C.
Advantageously, in step C), the second layer comprises above 50%, more preferably above 75% of zinc and advantageously above 90% of zinc. The second layer can be deposited by any deposition method known by the man skilled in the art. It can be by hot-dip coating, by vacuum deposition or by electro-galvanizing.
For example, the coating based on zinc comprises from 0.01 to 8.0% Al, optionally 0.2-8.0% Mg, the remainder being Zn.
5 PCT/IB2018/058154 Preferably, the coating based on zinc is deposited by hot-dip galvanizing. In this embodiment, the molten bath can also comprise unavoidable impurities and residuals elements from feeding ingots or from the passage of the steel sheet in the molten bath. For example, the optionally impurities are chosen from Sr, Sb, 5 Pb, Ti, Ca, Mn, Sn, La, Ce, Cr, Zr or Bi, the content by weight of each additional element being inferior to 0.3% by weight. The residual elements from feeding ingots or from the passage of the steel sheet in the molten bath can be iron with a content up to 5.0%, preferably 3.0%, by weight.
In a preferred embodiment, the second layer consists of zinc. When the coating is deposited by hot-dip galvanizing, the percentage of Al is comprised between 0.15 and 0.40 wt.% in the bath. Moreover, the iron presents in the first coating reacts with aluminum in order to form the inhibition layer Fe2A15 and thus provide reactive wetting behavior during hot dip galvanizing.
With the method according to the present invention, a steel sheet coated with a diffused alloy layer comprising iron and nickel, such layer being directly topped by a zinc based layer is obtained. It is believed that the diffused alloy layer acts like a barrier layer to LME and improves the coating adhesion.
Preferably, the steel sheet has a microstructure comprising from 1 to 50%
of residual austenite, from 1 to 60% of martensite and optionally at least one element chosen from: bainite, ferrite, cementite and pearlite. In this case, the martensite can be tempered or untempered.
In a preferred embodiment, the steel sheet has a microstructure comprising from 5 to 25 % of residual austenite.
Preferably, the steel sheet has a microstructure comprising from 1 to 60%
and more preferably between 10 to 60% of tempered martensite.
Advantageously, the steel sheet has a microstructure comprising from 10 to 40% of bainite, such bainite comprising from 10 to 20% of lower bainite, from 0 to 15% of upper bainite and from 0 to 5% of carbide free bainite.
Preferably, the steel sheet has a microstructure comprising from 1 to 25%
of ferrite.
Preferably, the steel sheet has a microstructure comprising from 1 to 15%
untempered martensite.
In a preferred embodiment, the second layer consists of zinc. When the coating is deposited by hot-dip galvanizing, the percentage of Al is comprised between 0.15 and 0.40 wt.% in the bath. Moreover, the iron presents in the first coating reacts with aluminum in order to form the inhibition layer Fe2A15 and thus provide reactive wetting behavior during hot dip galvanizing.
With the method according to the present invention, a steel sheet coated with a diffused alloy layer comprising iron and nickel, such layer being directly topped by a zinc based layer is obtained. It is believed that the diffused alloy layer acts like a barrier layer to LME and improves the coating adhesion.
Preferably, the steel sheet has a microstructure comprising from 1 to 50%
of residual austenite, from 1 to 60% of martensite and optionally at least one element chosen from: bainite, ferrite, cementite and pearlite. In this case, the martensite can be tempered or untempered.
In a preferred embodiment, the steel sheet has a microstructure comprising from 5 to 25 % of residual austenite.
Preferably, the steel sheet has a microstructure comprising from 1 to 60%
and more preferably between 10 to 60% of tempered martensite.
Advantageously, the steel sheet has a microstructure comprising from 10 to 40% of bainite, such bainite comprising from 10 to 20% of lower bainite, from 0 to 15% of upper bainite and from 0 to 5% of carbide free bainite.
Preferably, the steel sheet has a microstructure comprising from 1 to 25%
of ferrite.
Preferably, the steel sheet has a microstructure comprising from 1 to 15%
untempered martensite.
6 After the manufacture of a steel sheet, in order to produce some parts of a vehicle, it is known to assembly by welding two metal sheets. Thus, a spot welded joint is formed during the welding of at least two metal sheets, said spot being the link between the at least two metal sheets.
To produce a spot welded joint according to the invention, the welding is performed with an effective intensity is between 3kA and 15kA and the force applied on the electrodes is between 150 and 850 daN with said electrode active face diameter being between 4 and lOmm.
Thus, a spot welded joint of at least two metal sheets, comprising the coated steel sheet according to the present invention, is obtained, such said joint containing less than 3 cracks having a size above 100 m and wherein the longest crack has a length below 500 m.
Preferably, the second metal sheet is a steel sheet or an aluminum sheet.
More preferably, the second metal sheet is a steel sheet according to the present invention.
In another embodiment, the spot welded joint comprises a third metal sheet being a steel sheet or an aluminum sheet. For example, the third metal sheet is a steel sheet according to the present invention.
The steel sheet or the spot welded joint according to the present invention can be used for the manufacture of parts for automotive vehicle.
The invention will now be explained in trials carried out for information only.
They are not limiting.
Example For all samples, steel sheets used have the following composition in weight percent: C=0.37%, Mn=1.9 wt.%, Si=1.9 wt.%, Cr=0.35 wt.%, AI=0.05 wt.% and Mo=0.1 wt.%.
Trial 1 and 2 were prepared by deposited a first coating comprising 45% of Fe, the balance being Ni. Then, a continuous annealing was performed in an atmosphere comprising 5% of H2 and 95% of N2 at a dew point of -45 C. The pre-coated steel sheet was heated at a temperature of 900 C. Finally, a zinc coating
To produce a spot welded joint according to the invention, the welding is performed with an effective intensity is between 3kA and 15kA and the force applied on the electrodes is between 150 and 850 daN with said electrode active face diameter being between 4 and lOmm.
Thus, a spot welded joint of at least two metal sheets, comprising the coated steel sheet according to the present invention, is obtained, such said joint containing less than 3 cracks having a size above 100 m and wherein the longest crack has a length below 500 m.
Preferably, the second metal sheet is a steel sheet or an aluminum sheet.
More preferably, the second metal sheet is a steel sheet according to the present invention.
In another embodiment, the spot welded joint comprises a third metal sheet being a steel sheet or an aluminum sheet. For example, the third metal sheet is a steel sheet according to the present invention.
The steel sheet or the spot welded joint according to the present invention can be used for the manufacture of parts for automotive vehicle.
The invention will now be explained in trials carried out for information only.
They are not limiting.
Example For all samples, steel sheets used have the following composition in weight percent: C=0.37%, Mn=1.9 wt.%, Si=1.9 wt.%, Cr=0.35 wt.%, AI=0.05 wt.% and Mo=0.1 wt.%.
Trial 1 and 2 were prepared by deposited a first coating comprising 45% of Fe, the balance being Ni. Then, a continuous annealing was performed in an atmosphere comprising 5% of H2 and 95% of N2 at a dew point of -45 C. The pre-coated steel sheet was heated at a temperature of 900 C. Finally, a zinc coating
7 was deposited by hot-dip galvanizing, the zinc bath comprising 0.2% of Al. The bath temperature was of 460 C.
For comparison purpose, Trial 3 was prepared by depositing a zinc coating by electro-galvanizing after the continuous annealing of the above steel sheet.
The resistance to LME of Trials 1 to 3 was evaluated. To this end, for each Trial, two coated steel sheets were welded together by resistance spot welding.
The type of the electrode was ISO Type B with a diameter of 16mm; the force of the electrode was of 5kN and the flow rate of water of was 1.5g/min. the welding cycle is reported in Table 1.
Table 1. Welding Schedule Weld time Pulses Pulse (cy) Cool time (cy) Hold time (cy) Cycle 2 12 2 10 The number of cracks above 100 m was then evaluated using an optical as well as SEM (Scanning Electron Microscopy as reported in Table 2.
Table 2. LME crack details after spot welding (2 layer stack-up condition) Number of Maximum cracks crack 2nd Thickness Trials 1st coating Thickness (> 100 m) length (1-1m) coating (1-1m) per spot (1-1m) weld Trial 1* Fe - (55`)/0)Ni 1 Zn (GI) 7 0 0 Trial 2* Fe - (55`)/0)Ni 2 Zn (GI) 7 0 0 Trial 3 - _ Zn (EG) 7 3 760 *: according to the present invention.
Trials according to the present invention show an excellent resistance to LME compared to Trial 3.
Then, for each Trial, three coated steel sheets were welded together by resistance spot welding under three layer stack-up configuration. The number of
For comparison purpose, Trial 3 was prepared by depositing a zinc coating by electro-galvanizing after the continuous annealing of the above steel sheet.
The resistance to LME of Trials 1 to 3 was evaluated. To this end, for each Trial, two coated steel sheets were welded together by resistance spot welding.
The type of the electrode was ISO Type B with a diameter of 16mm; the force of the electrode was of 5kN and the flow rate of water of was 1.5g/min. the welding cycle is reported in Table 1.
Table 1. Welding Schedule Weld time Pulses Pulse (cy) Cool time (cy) Hold time (cy) Cycle 2 12 2 10 The number of cracks above 100 m was then evaluated using an optical as well as SEM (Scanning Electron Microscopy as reported in Table 2.
Table 2. LME crack details after spot welding (2 layer stack-up condition) Number of Maximum cracks crack 2nd Thickness Trials 1st coating Thickness (> 100 m) length (1-1m) coating (1-1m) per spot (1-1m) weld Trial 1* Fe - (55`)/0)Ni 1 Zn (GI) 7 0 0 Trial 2* Fe - (55`)/0)Ni 2 Zn (GI) 7 0 0 Trial 3 - _ Zn (EG) 7 3 760 *: according to the present invention.
Trials according to the present invention show an excellent resistance to LME compared to Trial 3.
Then, for each Trial, three coated steel sheets were welded together by resistance spot welding under three layer stack-up configuration. The number of
8 cracks above 100 m was then evaluated using an optical as well as SEM
(Scanning Electron Microscopy) as reported in Table 3.
Table 3. LME crack details after spot welding (3 layer stack-up condition) Number of cracks Maximum crack length Trials (> 100 m) per spot weld (1-1m) Trial 1* 1 250 Trial 2* 1 450 Trial 3 7 850 *: according to the present invention.
Trials according to the present invention show an excellent resistance to LME as compared to Trial 3.
Finally, Trials 1 and 2 were bent at a 900 angle followed. An adhesive tape was then applied and removed to verify the coating adhesion with the substrate steel. The coating adhesion of those Trials was excellent.
(Scanning Electron Microscopy) as reported in Table 3.
Table 3. LME crack details after spot welding (3 layer stack-up condition) Number of cracks Maximum crack length Trials (> 100 m) per spot weld (1-1m) Trial 1* 1 250 Trial 2* 1 450 Trial 3 7 850 *: according to the present invention.
Trials according to the present invention show an excellent resistance to LME as compared to Trial 3.
Finally, Trials 1 and 2 were bent at a 900 angle followed. An adhesive tape was then applied and removed to verify the coating adhesion with the substrate steel. The coating adhesion of those Trials was excellent.
Claims (30)
1. Method for the manufacture of a coated steel sheet comprising the following step:
A. the provision of a pre-coated steel sheet coating with a first coating comprising iron and nickel, B. the thermal treatment of such pre-coated steel sheet at a temperature between 600 and 1000°C, C. the coating of the steel sheet obtained in step B) with a second coating based on zinc.
A. the provision of a pre-coated steel sheet coating with a first coating comprising iron and nickel, B. the thermal treatment of such pre-coated steel sheet at a temperature between 600 and 1000°C, C. the coating of the steel sheet obtained in step B) with a second coating based on zinc.
2. Method according to claim 1, wherein in step A), the first coating comprises from 10% to 75% by weight of iron.
3. Method according to claim 2, wherein in step A), the first coating comprises from 25 to 65 % by weight of iron.
4. Method according to anyone of claims 1 to 3, wherein in step A), the first coating comprises from 40 to 60% of weight of iron.
5. Method according to anyone of claims 1 to 4, wherein in step A), the first coating comprises from 25 to 90% by weight of nickel.
6. Method according to claim 5, wherein in step A), the first coating comprises from 35 to 75 % by weight of nickel.
7. Method according to claim 6, wherein in step A), the first coating comprises from 40 to 60% by weight of nickel.
8. Method according to anyone of claims 1 to 7, wherein in step A), the first coating consists of iron and nickel.
9. Method according to anyone of claims 1 to 8, wherein in step A), the first coating has a thickness equal or above 0.5 µm.
10. Method according to claim 9, wherein in step A), the first coating has a thickness between 0.8 and 5.0 µm.
11. Method according to claim 10, wherein in step A), the first coating has a thickness between 1.0 and 2.0µm.
12. Method according to anyone of claim 1 to 11, wherein in step A), the steel sheet composition comprises:
0.10 < C < 0.40%, 1.5 < Mn < 3.0%, 0.7 < Si < 2.0%, 0.05 < Al < 1.0%
0.75 < (Si+Al) < 3.0 %
and on a purely optional basis, one or more elements such as Nb 0.5 %, B 0.005%, Cr 1.0%, Mo 0.50%, Ni 1.0%
Ti 0.5%, the remainder of the composition making up of iron and inevitable impurities resulting from the elaboration.
0.10 < C < 0.40%, 1.5 < Mn < 3.0%, 0.7 < Si < 2.0%, 0.05 < Al < 1.0%
0.75 < (Si+Al) < 3.0 %
and on a purely optional basis, one or more elements such as Nb 0.5 %, B 0.005%, Cr 1.0%, Mo 0.50%, Ni 1.0%
Ti 0.5%, the remainder of the composition making up of iron and inevitable impurities resulting from the elaboration.
13. Method according to anyone of claims 1 to 12, wherein in step C), the second layer comprises above 50% of zinc.
14. Method according to claim 13, wherein in step C), the second layer comprises above 75% of zinc.
15. Method according to claim 14, wherein in step C), the second layer comprises above 90% of zinc.
16. Method according to claim 15, wherein in step C), the second layer consists of zinc.
17. Method according to anyone of claims 1 to 16, wherein in step B), the thermal treatment is a continuous annealing.
18. Method according to anyone of claims 1 to 17, wherein in step B), the thermal treatment is performed in an atmosphere comprising from 1 to 30% of H2 at a dew point between -10 and -60°C.
19. A steel sheet obtainable from the method according to anyone of claims 1 to 18 coated with a diffused alloy layer comprising iron and nickel, such layer being directly topped by a zinc based layer.
20. Steel sheet according to claim 19, wherein the steel microstructure comprises from 1 to 50% of residual austenite, from 1 to 60% of martensite and optionally at least one element chosen from: bainite, ferrite, cementite and pearlite.
21. Steel sheet according to claim 20, wherein the microstructure comprises from to 25 % of residual austenite.
22. Steel sheet according to claim 20 or 21, wherein the microstructure comprises from 1 to 60% of tempered martensite.
23. Steel sheet according to anyone of claims 20 to 22, wherein the microstructure comprises from 10 to 40% of bainite.
24. Steel sheet according to anyone of claims 20 to 23, wherein the microstructure comprises from 1 to 25% of ferrite.
25. Steel sheet according to anyone of claims 20 to 24, wherein the microstructure comprises from 1 to 15% of untempered martensite.
26.Spot welded joint of at least two metal sheets comprising at least a steel sheet according to anyone of claims 19 to 25 or obtainable from the method according to anyone of claims 1 to 18, said joint containing less than 3 cracks having a size above 100µm and wherein the longest crack has a length below 500µm.
27.Spot welded joint according to claim 26, wherein the second metal sheet is a steel sheet or an aluminum sheet.
28.Spot welded joint according to claim 27, wherein the second metal sheet is a steel sheet according to anyone of claims 19 to 25 or obtainable from the method according to claims 1 to 18.
29.Spot welded joint according to anyone of claims 26 to 28, comprising a third metal sheet being a steel sheet or an aluminum sheet.
30. Use of a coated steel sheet according to anyone of claims 19 to 25 or a spot welded point according to anyone of claims 26 to 29, for the manufacture of part for automotive vehicle.
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CN111279007B (en) | 2017-10-24 | 2023-01-24 | 安赛乐米塔尔公司 | Method for manufacturing zinc-plated diffusion-annealed steel sheet |
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